US1352743A - Fluid-pressure motor - Google Patents

Fluid-pressure motor Download PDF

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US1352743A
US1352743A US344561A US34456119A US1352743A US 1352743 A US1352743 A US 1352743A US 344561 A US344561 A US 344561A US 34456119 A US34456119 A US 34456119A US 1352743 A US1352743 A US 1352743A
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pressure
chamber
turbine
fluid
valve
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Hall Thomas
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups

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  • My invention relates to elastic fluid turbines, particularly steam turbines, and still more particularly to means for reducing to a minimum inflow of air and outflow of'working fluid through stuffing boxes of such turbines.
  • My invention comprisesmeans for maintaining a substantially constant low pressure in an intermediate portion of such a stufling box, and in other features all as hereinafter described and particularly pointed out in the appended claims.
  • the objects of my invention are to avoid the drawing of air into the turbine through its stufling'box, and also to avoid or reduce to a minimum the escape of steam or other working fluid through such stuffing box, and to accomplish such objects in a simple man ner, and by inexpensive means.
  • Figure 1 shows an axial vertical section of a steam turbine of well known type with my invention added thereto, the illustration of such invention being more or less diagram-' matic.
  • Fig. 2 shows a longitudinal section of the regulating valve.
  • FIG. 1 designates the motor of the turbine, the stator, of which the casing 3 is a part, 4, 5, 6-12 inclusive designate successive sta es of the turbine, and 15 the exhaust cham er of the turbine.
  • 16 designates the highipressure stufling box; which comprises chambers J, K and L. Between chamber L and the highest pressure stage of the turbine there is a suitable packing 19 hearing against the periphery of the turbine rotor, the nature of which packing it is not necessary to describe here; between chambers L and K there is another similar packing 18, and between chambers K and J there is another similar packing 17.
  • Chamber K is customarily connected by a duct 30 to a suitable low pressure stage of the turbine, so that steam may pass from chamber K into that stage and may be there utilized. Now these packings, while they greatly reduce leakage of steam outward and flow of air inward, do not. altogether prevent such leakage or flow. There may be some leakage of steam from the highest stage of the turbine into chamber L, and
  • an automatic pressureregulating reliei valve 20 which is loaded with the pres sure of the exhaust of the turbine or some other stage of the turbine so low as to be practically a constant pressure under all loads; this loading being increased by a spring or other suitable substantially constant and readily re lable means, to the end that said valve wi 1 open to-relieve pressure in chamber K whenever the pressure in said chamber exceeds the loading of the valve and will close'when the pressure in chamber K falls to the predetermined intended pressure.
  • valve 20 The construction of the valve 20 is simple. It comprises a seat-bushing 21, screwed into a suitable aperture in the turbine casing 3; a sliding valve-proper 22 within said bushing 21; a valve bonnet 23, a loading spring 24 and a regulating screw 25, cus tomarily covered by a cap 26. Suitable packings are provided to prevent escape of steam at the base of the cap 26, and at the base of the bonnet 23. At a convenient point in the bonnet 23 there is connected aduct 27 leading to the exhaust chamber of the turbine or, it may be, to one of the lowest stages of the turbine; in any case, leading to predetermined pressure.
  • valve proper 22 seats against a suitable seating-portion of the bushing 21, such seating-portion surrounding a port 28 connecting with chamber K; and in the sides of bushing 21 there are ports 29 leading to a relief duct 30 which is the customary duct leading to a suitable low pressure stage of the turbine.
  • this automatic relief valve I employ, as is common, a reducing valve 31, in a pipe line 32 leading to chamber K from some source of supply (for example, the main steam line) which may be relied upon for steam pressure greater than that to be maintained in chamberK.
  • a reducing valve 31 in a pipe line 32 leading to chamber K from some source of supply (for example, the main steam line) which may be relied upon for steam pressure greater than that to be maintained in chamberK.
  • the purpose of this reducing valve is, as usual, to maintain in chamber a certain definite pressure, above that of the atmosphere.
  • This the reducing valve may do on low loads; but if, when the turbine is running on heavy loads, the leakage from the high pressure side of the turbine through chamber L'becomes so great as to maintain in chamber K a higher pressure than that for which the reducing valve is set, then, as before stated, except for this relief valve 20, leakage of steam will occur from chamber K to chamber J and thence to the atmosphere, with the resultant loss of considerable steam. But such loss is prevented by the relief valve 20, which, when the pressure in K is higher than that for which the relief valve is set, will open, discharging to a suitable low pressure stage of the turbine to which duct 30 is connected, in which the steam thus escaping from chamber K is utilized. On the other hand, relief valve 20 closes romptly when the pressure in chamber K falls to that corresponding to theloading of the valve, so preventing entrance of air.
  • the loading of the valve 20 is extremely uniform, and the valve 20 may be relied upon to open promptly when the pressure in K rises above the predetermined pressure, and to close promptly when the pressure in chamber K falls to the Since most turbines are operated condensing, the spring 24 is commonly adjusted so that the valve 20 will open only when the pressure in K exceeds some pressure'higher than atmospheric pressureusua1ly about five pounds above atmosphere. When the turbine is run non-condensing, this pressure for which valve 20 is set may be somewhat higher.
  • a'turbine comprising a stator and a rotor, of a high pres- ,sure packing for the joint between the rotor and stator comprising a pluralitypf chambers, one arranged to receive leaking steam from the turbine, another exposed to indrawn air, and a third chamber exposed to charge, said-relief valve having fluid-pressure-actuated loading means supplied with working fluid by"connection to the exhaust of the turbine, together with supplemental loading means tending to hold said valve closed up to a predetermined pressure higher than the normal exhaust pressure.

Description

warren srrss THOMAS HALL, OF HARRISBURG, PENNSYLVANIA.
FLUID-PRESSURE Moron.
Specification of Letters Patent. Patented S pt 14 1920. I
Application filed December 13, 1919. Serial 310.344,!561.
To all whom it may concern:
Be it known that I, THOMAS HALL, citizen of the United States of America, and a resident of Harrisburg, Dauphin'county, Pennsylvania, have invented certain new and useful Improvements in Fluid-Pressure Motors, of which the following is a specification.
My invention relates to elastic fluid turbines, particularly steam turbines, and still more particularly to means for reducing to a minimum inflow of air and outflow of'working fluid through stuffing boxes of such turbines. My invention comprisesmeans for maintaining a substantially constant low pressure in an intermediate portion of such a stufling box, and in other features all as hereinafter described and particularly pointed out in the appended claims.
The objects of my invention are to avoid the drawing of air into the turbine through its stufling'box, and also to avoid or reduce to a minimum the escape of steam or other working fluid through such stuffing box, and to accomplish such objects in a simple man ner, and by inexpensive means.
I will now proceed to describe my invention with reference to the accompanying drawings and will then point out the novel features in claims.
Figure 1 shows an axial vertical section of a steam turbine of well known type with my invention added thereto, the illustration of such invention being more or less diagram-' matic.
Fig. 2 shows a longitudinal section of the regulating valve. I
In the drawings 1 designates the motor of the turbine, the stator, of which the casing 3 is a part, 4, 5, 6-12 inclusive designate successive sta es of the turbine, and 15 the exhaust cham er of the turbine. 16 designates the highipressure stufling box; which comprises chambers J, K and L. Between chamber L and the highest pressure stage of the turbine there is a suitable packing 19 hearing against the periphery of the turbine rotor, the nature of which packing it is not necessary to describe here; between chambers L and K there is another similar packing 18, and between chambers K and J there is another similar packing 17. Chamber K is customarily connected by a duct 30 to a suitable low pressure stage of the turbine, so that steam may pass from chamber K into that stage and may be there utilized. Now these packings, while they greatly reduce leakage of steam outward and flow of air inward, do not. altogether prevent such leakage or flow. There may be some leakage of steam from the highest stage of the turbine into chamber L, and
thence" into chamber K, and thence, par
ticularly when the turbine is working under heavy load, from chamber K to chamber 'J and thence to the outside air; and, conversely, particularly when the turbine is working condensing, and under light load, there may be leakage of air into chamber J, thence into chamber K, and thence through the said duct 30 connecting that chamber K with a low pressure stage of the turbine,
to the condenser into which the turbine ex-' chamber to a low pressure stage of the turbine, an automatic pressureregulating reliei valve 20 which is loaded with the pres sure of the exhaust of the turbine or some other stage of the turbine so low as to be practically a constant pressure under all loads; this loading being increased by a spring or other suitable substantially constant and readily re lable means, to the end that said valve wi 1 open to-relieve pressure in chamber K whenever the pressure in said chamber exceeds the loading of the valve and will close'when the pressure in chamber K falls to the predetermined intended pressure.
The construction of the valve 20 is simple. It comprises a seat-bushing 21, screwed into a suitable aperture in the turbine casing 3; a sliding valve-proper 22 within said bushing 21; a valve bonnet 23, a loading spring 24 and a regulating screw 25, cus tomarily covered by a cap 26. Suitable packings are provided to prevent escape of steam at the base of the cap 26, and at the base of the bonnet 23. At a convenient point in the bonnet 23 there is connected aduct 27 leading to the exhaust chamber of the turbine or, it may be, to one of the lowest stages of the turbine; in any case, leading to predetermined pressure.
a point such that the pressure is substantially constant whatever may be the load on the turbine.
The valve proper 22 seats against a suitable seating-portion of the bushing 21, such seating-portion surrounding a port 28 connecting with chamber K; and in the sides of bushing 21 there are ports 29 leading to a relief duct 30 which is the customary duct leading to a suitable low pressure stage of the turbine.
In connection with this automatic relief valve I employ, as is common, a reducing valve 31, in a pipe line 32 leading to chamber K from some source of supply (for example, the main steam line) which may be relied upon for steam pressure greater than that to be maintained in chamberK. The purpose of this reducing valve is, as usual, to maintain in chamber a certain definite pressure, above that of the atmosphere. This the reducing valve may do on low loads; but if, when the turbine is running on heavy loads, the leakage from the high pressure side of the turbine through chamber L'becomes so great as to maintain in chamber K a higher pressure than that for which the reducing valve is set, then, as before stated, except for this relief valve 20, leakage of steam will occur from chamber K to chamber J and thence to the atmosphere, with the resultant loss of considerable steam. But such loss is prevented by the relief valve 20, which, when the pressure in K is higher than that for which the relief valve is set, will open, discharging to a suitable low pressure stage of the turbine to which duct 30 is connected, in which the steam thus escaping from chamber K is utilized. On the other hand, relief valve 20 closes romptly when the pressure in chamber K falls to that corresponding to theloading of the valve, so preventing entrance of air.
Since'the pressure communicated through duct 27 to the loading side of the valve 20 is extremely uniform, the loading of the valve is extremely uniform, and the valve 20 may be relied upon to open promptly when the pressure in K rises above the predetermined pressure, and to close promptly when the pressure in chamber K falls to the Since most turbines are operated condensing, the spring 24 is commonly adjusted so that the valve 20 will open only when the pressure in K exceeds some pressure'higher than atmospheric pressureusua1ly about five pounds above atmosphere. When the turbine is run non-condensing, this pressure for which valve 20 is set may be somewhat higher.
What I claim is:
1. The combination with a turbine comprising successive stages of progressively lower pressures, of a packing chamber, a
duct connecting said chamber to a low pressure stage of the turbine, a self-opening relief valve in said duct between said chamber and said low pressure stage, said relief valve having loading means tending to prevent its opening below the pressure to be maintained in said chamber, and to cause it to close when the pressure in such chamber falls to a predetermined pressure, and means for supplying working fluid at a predetermined pressure to saidbchamber.
2. The combination with a turbine comprising successive stages of progressively lower pressures, of a packing chamber, a duct connecting said chamber to a low pres sure stage of the turbine, a relief valve in said duct between said chamber and said low pressure stage, said relief valve having fluid-pressure-actuated loading means connectedto a source of substantiallyconstant low fluid pressure, and having also other loading means preventing the opening of said relief valve below a pressure higher than such low'pressure, said loading means arranged to cause said relief valve to close when the pressure in such chamber falls to a predetermined pressure, and means for supplying working fluid at a predetermined pressure to said chamber.
3. The combination with a turbine comprising successive stages of progressively lower pressures, of a packing chamber, a duct connecting said chamber to a low pressure stage of the turbine, a relief valve in said duct between said chamber and said low pressure stage, said relief valve having fluid-pressure-actuated loading means connected to the exhaust pressure of the turbine, and having also other loading means preventing the opening of said relief valve below a pressure higher than such exhaust pressure, said loading means arranged to cause said relief valve to close when the pressure in such chamber falls to a predetermined pressure, and means for supplying working fluid at a predetermined pressure to said chamber.
4. The combination with a turbine comprising a stator and a rotor, of a high pressure packing for the joint between the rotor and stator comprising a, plurality of chambers, one arranged to receive leaking steam from the turbine, another exposed to indrawn air, and a third chamber exposed to leakage from said previously mentioned chambers, means for supplying to said intermediate chamber working fluid at a predetermined pressure, a duct for conveying working fluid from said intermediate chamber to a suitable discharge point in the turbine, and a relief valve between said intermediate chamber and said point of discharge, said relief valve having loading means tending to prevent its opening below the pressure to be maintained in said intermediate chamber, and to cause 'to close when the pressure in such intermediate chamber falls .to a predetermined pressure. 5. The combination with a'turbine comprising a stator and a rotor, of a high pres- ,sure packing for the joint between the rotor and stator comprising a pluralitypf chambers, one arranged to receive leaking steam from the turbine, another exposed to indrawn air, and a third chamber exposed to charge, said-relief valve having fluid-pressure-actuated loading means supplied with working fluid by"connection to the exhaust of the turbine, together with supplemental loading means tending to hold said valve closed up to a predetermined pressure higher than the normal exhaust pressure.
6. The combination with a fluid-pressure mined limit, of a relief passage for said chamber and a relief valve'therein compris engine comprising a chamber in which p res sure 1s to be maintamed above a predetering fluid-pressure-actuated loading means. connected to the exhaust of said engine; as
constituting an approximately uniform source of lowpressure loading fluid.
7. The combination with a fluid-pressure engine comprising a chamber in which pressure is to be maintained above a predetermined limit, of a relief passage for 'said chamber and a relief valve therein comprising fluid-pressure-actuated [loading means connected to the exhaust of said engine as constituting an approximately funiform source of low pressure loading fluid, and comprising also supplemental .-loading means.
In testimony whereof I have signed this specification in the presence of two subscribing witnesses. a
THOMAS HALL.
Witnesses:
MARY vE. RINEARD, W. M. Ross;
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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2463898A (en) * 1944-11-24 1949-03-08 Wright Aeronautical Corp Turbine sealing construction
US2495525A (en) * 1943-11-03 1950-01-24 Worthington Pump & Mach Corp Circulating pump for steam generators
US2614797A (en) * 1947-03-10 1952-10-21 Ingersoll Rand Co Pressure fluid seal controlling device
US3014694A (en) * 1954-10-25 1961-12-26 Garrett Corp Gas turbine and sealing means therefor

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2495525A (en) * 1943-11-03 1950-01-24 Worthington Pump & Mach Corp Circulating pump for steam generators
US2463898A (en) * 1944-11-24 1949-03-08 Wright Aeronautical Corp Turbine sealing construction
US2614797A (en) * 1947-03-10 1952-10-21 Ingersoll Rand Co Pressure fluid seal controlling device
US3014694A (en) * 1954-10-25 1961-12-26 Garrett Corp Gas turbine and sealing means therefor

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